Cranfield report Aero

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Bibliographische Detailangaben
Körperschaft: Cranfield Institute of Technology (Herausgebendes Organ)
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Veröffentlicht: Cranfield 1970-
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Monografische Reihe
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Titel Jahr Band
On the adequate model for aircraft parameter estimation 1975 28
The influence of short springs on longitudinal static stability 1975 29
Parameter identification applied to aircraft 1974 26
Subsonic jet transport noise : the relative importance of various parameters 1974 25
A proposal for a self-contained instrumentation system for flight research on stability and control 1974 21
Application of the Fokker-Planck equation to random vibration of nonlinear systems 1974 20
The weight, econimic and noise penalties of short haul transport aircraft resulting from the reduction of balanced field length 1974 24
Longitudinal aerodynamic derivates of a slender delta-wing research aircraft extracted from flight data 1974 27
A performance test survey of the aerodynamic development of the Slingsby T51 Dart Sailplane 1973 16
Analysis of taxying induced vibrations in aircraft by the power spectral density method 1973 15
Progress report on an investigation of a non-planar vortex lattice method for wing calculations 1973 17
Performance characteristics of short haul transport aircraft intended to operate from reduced length runways 1973 18
Aircraft design studies - E67 : tilt-wing executive aircraft 1973 23
Additional damping for tall structures 1973 19
Evaluation of the basic performance characteristics of an instrumentation sytem 1973 22
Aeroplane design study STOL airliner (A71) Pt. 1 Configuration description and data / by D. Howe and R. E. Ward 1972 12
Aeroplane design study STOL airliner (A71) Pt. 2 Detail design features / by D. Howe 1972 13
A comparative assessment of three methods of measurement of pressure error corrections 1972 11
The design of a shaft cross coupling system for the engines of an STOL aircraft 1972 14
A computer simulation of pilot activity during the blind landing of an airliner 1971 4
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